In Section5.4 we derived the differential equation
mx″+cx′+kx=F(t)
mx''+cx'+kx=F(t)
(1)
that governs the one-dimensional motion of a mass m that is attached to a spring (with constant k) and a dashpot (with constant c) and is also acted on by an external force F(t). Machines with rotating components commonly involve mass-spring systems (or their equivalents) in which the external force is simple harmonic:
F(t)=F0cosωtorF(t)=F0sinωt,
F(t)=F0cosωtorF(t)=F0sinωt,
(2)
where the constant F0F0 is the amplitude of the periodic force and ωω is its circular frequency.
For an example of how a rotating machine component can provide a simple harmonic force, consider the cart with a rotating vertical flywheel shown in Fig.5.6.1. The cart has mass m−m0,m−m0, not including the flywheel of mass m0.m0. The centroid of the flywheel is off center at a distance a from its center, and its angular speed is ωω radians per second. The cart is attached to a spring (with constant k) as shown. Assume that the centroid of the cart itself is directly beneath the center of the flywheel, and denote by x(t) its displacement from its equilibrium position (where the spring is unstretched). Figure5.6.1 helps us to see that the displacement ̲xx−− of the centroid of the combined cart plus flywheel is given by
ˉx=(m−m0)x+m0(x+acosωt)m=x+m0amcosωt.
x¯=(m−m0)x+m0(x+acosωt)m=x+m0amcosωt.
FIGURE5.6.1.
The cart-with-flywheel system.
Let us ignore friction and apply Newton’s second law m̲x″=−kx,mx−−''=−kx, because the force exerted by the spring is −kx.−kx. We substitute for ̲xx−− in the last equation to obtain
mx″−m0aω2cosωt=−kx;
mx''−m0aω2cosωt=−kx;
that is,
mx″+kx=m0aω2cosωt.
mx''+kx=m0aω2cosωt.
(3)
Thus the cart with its rotating flywheel acts like a mass on a spring under the influence of a simple harmonic external force with amplitude F0=m0aω2.F0=m0aω2. Such a system is a reasonable model of a front-loading washing machine with the clothes being washed loaded off center. This illustrates the practical importance of analyzing solutions of Eq.(1) with external forces as in (2).
Undamped Forced Oscillations
To study undamped oscillations under the influence of the external force F(t)=F0cosωt,F(t)=F0cosωt, we set c=0c=0 in Eq.(1), and thereby begin with the equation
mx″+kx=F0cosωt
mx''+kx=F0cosωt
(4)
whose complementary function is xc=c1cosω0t+c2sinω0t.xc=c1cosω0t+c2sinω0t. Here
ω0=√km
ω0=km−−−√
(as in Eq.(9) of Section5.4) is the (circular) natural frequency of the mass–spring system. The fact that the angle ω0tω0t is measured in (dimensionless) radians reminds us that if t is measured in seconds (s), then ω0ω0 is measured in radians per second—that is, in inverse seconds (s−1s−1). Also recall from Eq.(14) in Section5.4 that division of a circular frequency ωω by the number 2π2π of radians in a cycle gives the corresponding (ordinary) frequencyν=ω/2πν=ω/2π in Hz (hertz == cycles per second).
Let us assume initially that the external and natural frequencies are unequal: ω≠ω0.ω≠ω0. We substitute xp=Acosωtxp=Acosωt in Eq.(4) to find a particular solution. (No sine term is needed in xpxp because there is no term involving x′x' on the left-hand side in Eq.(4).) This gives
−mω2Acosωt+kAcosωt=F0cosωt,
−mω2Acosωt+kAcosωt=F0cosωt,
so
A=F0k−mω2=F0/mω20−ω2,
A=F0k−mω2=F0/mω20−ω2,
(5)
and thus
xp(t)=F0/mω20−ω2cosωt.
xp(t)=F0/mω20−ω2cosωt.
(6)
Therefore, the general solution x=xc+xpx=xc+xp is given by
x(t)=c1cosω0t+c2sinω0t+F0/mω20−ω2cosωt,
x(t)=c1cosω0t+c2sinω0t+F0/mω20−ω2cosωt,
(7)
where the constants c1c1 and c2c2 are determined by the initial values x(0)x(0) and x′(0).x'(0). Equivalently, as in Eq.(12) of Section5.4, we can rewrite Eq.(7) as
x(t)=Ccos(ω0t−α)+F0/mω20−ω2cosωt,
x(t)=Ccos(ω0t−α)+F0/mω20−ω2cosωt,
(8)
so we see that the resulting motion is a superposition of two oscillations, one with natural circular frequency ω0,ω0, the other with the frequency ωω of the external force.
Example1
Suppose that m=1,k=9,F0=80,m=1,k=9,F0=80, and ω=5,ω=5, so the differential equation in (4) is
x″+9x=80cos5t.
x''+9x=80cos5t.
Find x(t) if x(0)=x′(0)=0x(0)=x'(0)=0.
Solution
Here the natural frequency ω0=3ω0=3 and the frequency ω=5ω=5 of the external force are unequal, as in the preceding discussion. First we substitute xp=Acos5txp=Acos5t in the differential equation and find that −25A+9A=80,−25A+9A=80, so that A=−5.A=−5. Thus a particular solution is
xp(t)=−5cos5t.
xp(t)=−5cos5t.
The complementary function is xc=c1cos3t+c2sin3t,xc=c1cos3t+c2sin3t, so the general solution of the given nonhomogeneous equation is
x(t)=c1cos3t+c2sin3t−5cos5t,
x(t)=c1cos3t+c2sin3t−5cos5t,
with derivative
x′(t)=−3c1sin3t+3c2cos3t+25sin5t.
x'(t)=−3c1sin3t+3c2cos3t+25sin5t.
The initial conditions x(0)=0x(0)=0 and x′(0)=0x'(0)=0 now yield c1=5c1=5 and c2=0,c2=0, so the desired particular solution is
x(t)=5cos3t−5cos5t.
x(t)=5cos3t−5cos5t.
As indicated in Fig.5.6.2, the period of x(t) is the least common multiple 2π2π of the periods 2π/32π/3 and 2π/52π/5 of the two cosine terms.
FIGURE5.6.2.
The response x(t)=5cos3t−5cos5tx(t)=5cos3t−5cos5t in Example1.
Beats
If we impose the initial conditions x(0)=x′(0)=0x(0)=x'(0)=0 on the solution in (7), we find that
c1=−F0m(ω20−ω2)andc2=0,
c1=−F0m(ω20−ω2)andc2=0,
so the particular solution is
x(t)=F0m(ω20−ω2)(cosωt−cosω0t).
x(t)=F0m(ω20−ω2)(cosωt−cosω0t).
(9)
The trigonometric identity 2sinAsinB=cos(A−B)−cos(A+B),2sinAsinB=cos(A−B)−cos(A+B), applied with A=12(ω0+ω)tA=12(ω0+ω)t and B=12(ω0−ω)t,B=12(ω0−ω)t, enables us to rewrite Eq.(9) in the form
x(t)=F0m(ω20−ω2)sin12(ω0−ω)tsin12(ω0+ω)t.
x(t)=F0m(ω20−ω2)sin12(ω0−ω)tsin12(ω0+ω)t.
(10)
Suppose now that ω≈ω0,ω≈ω0, so that ω0+ωω0+ω is very large in comparison with |ω0−ω|.|ω0−ω|. Then sin12(ω0+ω)tsin12(ω0+ω)t is a rapidly varying function, whereas sin12(ω0−ω)tsin12(ω0−ω)t is a slowly varying function. We may therefore interpret Eq.(10) as a rapid oscillation with circular frequency 12(ω0+ω),12(ω0+ω),
x(t)=A(t)sin12(ω0+ω)t,
x(t)=A(t)sin12(ω0+ω)t,
but with a slowly varying amplitude
A(t)=2F0m(ω20−ω2)sin12(ω0−ω)t.
A(t)=2F0m(ω20−ω2)sin12(ω0−ω)t.
Example2
With m=0.1,F0=50,ω0=55,m=0.1,F0=50,ω0=55, and ω=45,ω=45,Eq.(10) gives
x(t)=sin5tsin50t.
x(t)=sin5tsin50t.
Figure5.6.3 shows the corresponding oscillation of frequency 12(ω0+ω)=5012(ω0+ω)=50 that is “modulated” by the amplitude function A(t)=sin5tA(t)=sin5t of frequency 12(ω0−ω)=512(ω0−ω)=5.
FIGURE5.6.3.
The phenomenon of beats.
A rapid oscillation with a (comparatively) slowly varying periodic amplitude exhibits the phenomenon of beats. For example, if two horns not exactly attuned to one another simultaneously play their middle C, one at ω0/(2π)=258ω0/(2π)=258 Hz and the other at ω/(2π)=254ω/(2π)=254 Hz, then one hears a beat—an audible variation in the amplitude of the combined sound—with a frequency of
(ω0−ω)/22π=258−2542=2(Hz).
(ω0−ω)/22π=258−2542=2(Hz).
Resonance
Looking at Eq.(6), we see that the amplitude A of xpxp is large when the natural and external frequencies ω0ω0 and ωω are approximately equal. It is sometimes useful to rewrite Eq.(5) in the form
A=F0k−mω2=F0/k1−(ω/ω0)2=±ρF0k,
A=F0k−mω2=F0/k1−(ω/ω0)2=±ρF0k,
(11)
where F0/kF0/k is the static displacement of a spring with constant k due to a constant force F0,F0, and the amplification factorρρ is defined to be
ρ=1|1−(ω/ω0)2|.
ρ=1|1−(ω/ω0)2|.
(12)
It is clear that ρ→+∞ρ→+∞ as ω→ω0.ω→ω0. This is the phenomenon of resonance—the increase without bound (as ω→ω0ω→ω0) in the amplitude of oscillations of an undamped system with natural frequency ω0ω0 in response to an external force with frequency ω≈ω0ω≈ω0.
We have been assuming that ω≠ω0.ω≠ω0. What sort of catastrophe should one expect if ωω and ω0ω0 are precisely equal? Then Eq.(4), upon division of each term by m, becomes
x″+ω20x=F0mcosω0t.
x''+ω20x=F0mcosω0t.
(13)
Because cosω0tcosω0t is a term of the complementary function, the method of undetermined coefficients calls for us to try
xp(t)=t(Acosω0t+Bsinω0t).
xp(t)=t(Acosω0t+Bsinω0t).
We substitute this in Eq.(13) and thereby find that A=0A=0 and B=F0/(2mω0).B=F0/(2mω0). Hence the particular solution is
xp(t)=F02mω0tsinω0t,
xp(t)=F02mω0tsinω0t,
(14)
The graph of xp(t)xp(t) in Fig.5.6.4 (in which m=1,F0=100,m=1,F0=100, and ω0=50ω0=50) shows vividly how the amplitude of the oscillation theoretically would increase without bound in this case of pure resonance, ω=ω0.ω=ω0. We may interpret this phenomenon as reinforcement of the natural vibrations of the system by externally impressed vibrations at the same frequency.
FIGURE5.6.4.
The phenomenon of resonance.
Example3
Cart with rotating flywheel Suppose that m=5 kgm=5 kg and k=500k=500 N/m in the cart with the flywheel of Fig.5.6.1. Then the natural frequency is ω0=√k/m=10ω0=k/m−−−−√=10 rad/s; that is, 10/(2π)≈1.5910/(2π)≈1.59 Hz. We would therefore expect oscillations of very large amplitude to occur if the flywheel revolves at about (1.59)(60)≈95(1.59)(60)≈95 revolutions per minute (rpm).
In practice, a mechanical system with very little damping can be destroyed by resonance vibrations. A spectacular example can occur when a column of soldiers marches in step over a bridge. Any complicated structure such as a bridge has many natural frequencies of vibration. If the frequency of the soldiers’ cadence is approximately equal to one of the natural frequencies of the structure, then—just as in our simple example of a mass on a spring—resonance will occur. Indeed, the resulting resonance vibrations can be of such large amplitude that the bridge will collapse. This has actually happened—for example, the collapse of Broughton Bridge near Manchester, England, in 1831—and it is the reason for the now-standard practice of breaking cadence when crossing a bridge. Resonance may have been involved in the 1981 Kansas City disaster in which a hotel balcony (called a skywalk) collapsed with dancers on it. The collapse of a building in an earthquake is sometimes due to resonance vibrations caused by the ground oscillating at one of the natural frequencies of the structure; this happened to many buildings in the Mexico City earthquake of September 19, 1985. On occasion an airplane has crashed because of resonant wing oscillations caused by vibrations of the engines. It is reported that for some of the first commercial jet aircraft, the natural frequency of the vertical vibrations of the airplane during turbulence was almost exactly that of the mass–spring system consisting of the pilot’s head (mass) and spine (spring). Resonance occurred, causing pilots to have difficulty in reading the instruments. Large modern commercial jets have different natural frequencies, so that this resonance problem no longer occurs.
Modeling Mechanical Systems
The avoidance of destructive resonance vibrations is an ever-present consideration in the design of mechanical structures and systems of all types. Often the most important step in determining the natural frequency of vibration of a system is the formulation of its differential equation. In addition to Newton’s law F=ma,F=ma, the principle of conservation of energy is sometimes useful for this purpose (as in the derivation of the pendulum equation in Section5.4). The following kinetic and potential energy formulas are often useful.
Kinetic energy:T=12mv2T=12mv2 for translation of a mass m with velocity v;
Kinetic energy:T=12Iω2T=12Iω2 for rotation of a body of a moment of inertia I with angular velocity ωω;
Potential energy:V=12kx2V=12kx2 for a spring with constant k stretched or compressed a distance x;
Potential energy:V=mghV=mgh for the gravitational potential energy of a mass m at height h above the reference level (the level at which V=0V=0), provided that g may be regarded as essentially constant.
Example4
Rolling disk Find the natural frequency of a mass m on a spring with constant k if, instead of sliding without friction, it is a uniform disk of radius a that rolls without slipping, as shown in Fig 5.6.5.
FIGURE5.6.5.
The rolling disk.
Solution
With the preceding notation, the principle of conservation of energy gives
12mv2+12Iω2+12kx2=E
12mv2+12Iω2+12kx2=E
where E is a constant (the total mechanical energy of the system). We note that v=aωv=aω and recall that I=ma2/2I=ma2/2 for a uniform circular disk. Then we may simplify the last equation to
34mv2+12kx2=E.
34mv2+12kx2=E.
Because the right-hand side of this equation is constant, differentiation with respect to t (with v=x′v=x' and v′=x″v'=x'') now gives
34mx′x″+kxx′=0.
34mx'x''+kxx'=0.
We divide each term by 32mx′32mx' to obtain
x″+2k3mx=0.
x′′+2k3mx=0.
Thus the natural frequency of horizontal back-and-forth oscillation of our rolling disk is √2k/3m,2k/3m−−−−−−√, which is √2/3≈0.81652/3−−−√≈0.8165 times the familiar natural frequency √k/mk/m−−−−√ of a mass on a spring that is sliding without friction rather than rolling without sliding. It is interesting (and perhaps surprising) that this natural frequency does not depend on the radius of the disk. It could be either a dime or a large disk with a radius of one meter (but of the same mass).
Example5
Car suspension Suppose that a car oscillates vertically as if it were a mass m=800 kgm=800 kg on a single spring (with constant k=7×104k=7×104 N/m), attached to a single dashpot (with constant c=3000 N·s/mc=3000 N⋅s/m). Suppose that this car with the dashpot disconnected is driven along a washboard road surface with an amplitude of 5 cm and a wavelength of L=10L=10 m (Fig.5.6.6). At what car speed will resonance vibrations occur?
We think of the car as a unicycle, as pictured in Fig.5.6.7. Let x(t) denote the upward displacement of the mass m from its equilibrium position; we ignore the force of gravity, because it merely displaces the equilibrium position as in Problem9 of Section5.4. We write the equation of the road surface as
y=acos2πsL(a=0.05 m, L=10 m).
y=acos2πsL(a=0.05 m, L=10 m).
(15)
When the car is in motion, the spring is stretched by the amount x−y,x−y, so Newton’s second law, F=ma,F=ma, gives
mx″=−k(x−y);
mx''=−k(x−y);
that is,
mx″=+kx=ky.
mx''=+kx=ky.
(16)
If the velocity of the car is v, then s=vts=vt in Eq.(15), so Eq.(16) takes the form
mx″=+kx=kacos2πvtL.
mx''=+kx=kacos2πvtL.
(16′)
This is the differential equation that governs the vertical oscillations of the car. In comparing it with Eq.(4), we see that we have forced oscillations with circular frequency ω=2πv/L.ω=2πv/L. Resonance will occur when ω=ω0=√k/m.ω=ω0=k/m−−−−√. We use our numerical data to find the speed of the car at resonance:
v=L2π√km=102π√7×104800≈14.89(m/s);
v=L2πkm−−−√=102π7×104800−−−−−−−√≈14.89(m/s);
that is, about 33.3 mi/h (using the conversion factor of 2.237 mi/h per m/s).
Damped Forced Oscillations
In real physical systems there is always some damping, from frictional effects if nothing else. The complementary function xcxc of the equation
mx″+cx′+kx=F0cosωt
mx''+cx'+kx=F0cosωt
(17)
is given by Eq.(19), (20), or (21) of Section5.4, depending on whether c>ccr=√4km,c=ccr,c>ccr=4km−−−−√,c=ccr, or c<ccr.c<ccr. The specific form is not important here. What is important is that, in any case, these formulas show that xc(t)→0xc(t)→0 as t→+∞.t→+∞. Thus xcxc is a transient solution of Eq.(17)—one that dies out with the passage of time, leaving only the particular solution xpxp.
The method of undetermined coefficients indicates that we should substitute
x(t)=Acosωt+Bsinωt
x(t)=Acosωt+Bsinωt
in Eq.(17). When we do this, collect terms, and equate coefficients of cosωtcosωt and sinωt,sinωt, we obtain the two equations
(k−mω2)A+cωB=F0,−cωA+(k−mω2)B=0
(k−mω2)A+cωB=F0,−cωA+(k−mω2)B=0
(18)
that we solve without difficulty for
A=(k−mω2)F0(k−mω2)2+(cω)2,B=cωF0(k−mω2)2+(cω)2.
A=(k−mω2)F0(k−mω2)2+(cω)2,B=cωF0(k−mω2)2+(cω)2.
(19)
If we write
Acosωt+Bsinωt=C(cosωtcosα+sinωtsinα)=Ccos(ωt−α)
Acosωt+Bsinωt=C(cosωtcosα+sinωtsinα)=Ccos(ωt−α)
as usual, we see that the resulting steady periodic oscillation
xp(t)=Ccos(ωt−α)
xp(t)=Ccos(ωt−α)
(20)
has amplitude
C=√A2+B2=F0√(k−mω2)2+(cω)2.
C=A2+B2−−−−−−−√=F0(k−mω2)2+(cω)2−−−−−−−−−−−−−−−√.
(21)
Now (19) implies that sinα=B/C>0,sinα=B/C>0, so it follows that the phase angle αα lies in the first or second quadrant. Thus
Note that if c>0,c>0, then the “forced amplitude”—defined as a function C(ω)C(ω) by (21)—always remains finite, in contrast with the case of resonance in the undamped case when the forcing frequency ωω equals the critical frequency ω0=√k/m.ω0=k/m−−−−√. But the forced amplitude may attain a maximum for some value of ω,ω, in which case we speak of practical resonance. To see if and when practical resonance occurs, we need only graph C as a function of ωω and look for a global maximum. It can be shown (Problem27) that C is a steadily decreasing function of ωω if c≧√2km.c≧2km−−−−√. But if c<√2km,c<2km−−−−√, then the amplitude of C attains a maximum value—and so practical resonance occurs—at some value of ωω less than ω0,ω0, and then approaches zero as ω→+∞.ω→+∞. It follows that an underdamped system typically will undergo forced oscillations whose amplitude is
Large if ωω is close to the critical resonance frequency;
Close to F0/kF0/k if ωω is very small;
Very small if ωω is very large.
Example6
Practical resonance Find the transient motion and steady periodic oscillations of a damped mass-and-spring system with m=1,c=2,m=1,c=2, and k=26k=26 under the influence of an external force F(t)=82cos4tF(t)=82cos4t with x(0)=6x(0)=6 and x′(0)=0.x'(0)=0. Also investigate the possibility of practical resonance for this system.
Solution
The resulting motion x(t)=xtr(t)+xsp(t)x(t)=xtr(t)+xsp(t) of the mass satisfies the initial value problem
x″+2x′+26x=82cos4t;x(0)=6,x′(0)=0.
x''+2x'+26x=82cos4t;x(0)=6,x'(0)=0.
(23)
Instead of applying the general formulas derived earlier in this section, it is better in a concrete problem to work it directly. The roots of the characteristic equation
r2+2r+26=(r+1)2+25=0
r2+2r+26=(r+1)2+25=0
are r=−1±5i,r=−1±5i, so the complementary function is
xc(t)=e−t(c1cos5t+c2sin5t).
xc(t)=e−t(c1cos5t+c2sin5t).
When we substitute the trial solution
x(t)=Acos4t+Bsin4t
x(t)=Acos4t+Bsin4t
in the given equation, collect like terms, and equate coefficients of cos 4t and sin 4t, we get the equations
10A+8B=82,−8A+10B=0
10A−8A++8B10B==82,0
with solution A=5,B=4.A=5,B=4. Hence the general solution of the equation in (23) is
x(t)=e−t(c1cos5t+c2sin5t)+5cos4t+4sin4t.
x(t)=e−t(c1cos5t+c2sin5t)+5cos4t+4sin4t.
At this point we impose the initial conditions x(0)=6,x′(0)=0x(0)=6,x'(0)=0 and find that c1=1c1=1 and c2=−3.c2=−3. Therefore, the transient motion and the steady periodic oscillation of the mass are given by
Figure5.6.8 shows graphs of the solution x(t)=xtr(t)+xsp(t)x(t)=xtr(t)+xsp(t) of the initial value problem
x″+2x′+26x=82cos4t,x(0)=x0,x′(0)=0
x''+2x'+26x=82cos4t,x(0)=x0,x'(0)=0
(24)
for the different values x0=−20,−10,0,10,x0=−20,−10,0,10, and 20 of the initial position. Here we see clearly what it means for the transient solution xtr(t)xtr(t) to “die out with the passage of time,” leaving only the steady periodic motion xsp(t).xsp(t). Indeed, because xtr(t)→0xtr(t)→0 exponentially, within a very few cycles the full solution x(t) and the steady periodic solution xsp(t)xsp(t) are virtually indistinguishable (whatever the initial position x0x0).
To investigate the possibility of practical resonance in the given system, we substitute the values m=1,c=2,m=1,c=2, and k=26k=26 in (21) and find that the forced amplitude at frequency ωω is
C(ω)=82√676−48ω2+ω4.
C(ω)=82676−48ω2+ω4−−−−−−−−−−−−−√.
The graph of C(ω)C(ω) is shown in Fig.5.6.9. The maximum amplitude occurs when
Thus practical resonance occurs when the external frequency is ω=√24ω=24−−√ (a bit less than the mass-and-spring’s undamped critical frequency of ω0=√k/m=√26ω0=k/m−−−−√=26−−√).
FIGURE5.6.8.
Solutions of the initial value problem in (24) with x0=−20,−10,0,10,x0=−20,−10,0,10, and 20.
FIGURE5.6.9.
Plot of amplitude C versus external frequency ωω.
5.6 Problems
In Problems 1 through 6, express the solution of the given initial value problem as a sum of two oscillations as in Eq.(8). Throughout, primes denote derivatives with respect to timet. In Problems 1–4, graph the solution functionx(t) in such a way that you can identify and label (as in Fig.5.6.2) its period.
mx″+kx=F0cosωtmx''+kx=F0cosωt with ω≠ω0;x(0)=x0,x′(0)=0ω≠ω0;x(0)=x0,x'(0)=0
mx″+kx=F0cosωtmx''+kx=F0cosωt with ω=ω0;x(0)=0,x′(0)=v0ω=ω0;x(0)=0,x'(0)=v0
In each of Problems 7 through 10, find the steady periodic solutionxsp(t)=Ccos(ωt−α)xsp(t)=Ccos(ωt−α)of the given equationmx″+cx′+kx=F(t)mx''+cx'+kx=F(t)with periodic forcing functionF(t) of frequencyω.ω.Then graphxsp(t)xsp(t)together with (for comparison) the adjusted forcing functionF1(t)=F(t)/mωF1(t)=F(t)/mω.
In each of Problems 11 through 14, find and plot both the steady periodic solutionxsp(t)=Ccos(ωt−α)xsp(t)=Ccos(ωt−α)of the given differential equation and the actual solutionx(t)=xsp(t)+xtr(t)x(t)=xsp(t)+xtr(t)that satisfies the given initial conditions.
Each of Problems 15 through 18 gives the parameters for a forced mass–spring–dashpot system with equationmx″+cx′+kx=F0cosωt.mx''+cx'+kx=F0cosωt.Investigate the possibility of practical resonance of this system. In particular, find the amplitudeC(ω)C(ω)of steady periodic forced oscillations with frequencyω.ω.Sketch the graph ofC(ω)C(ω)and find the practical resonance frequencyωω(if any).
m=1,c=2,m=1,c=2,k=2,k=2,F0=2F0=2
m=1,m=1,c=4,c=4,k=5,F0=10k=5,F0=10
m=1,c=6,m=1,c=6,k=45,k=45,F0=50F0=50
m=1,m=1,c=10,c=10,k=650,k=650,F0=100F0=100
A mass weighing 100 lb (mass m=3.125m=3.125 slugs in fps units) is attached to the end of a spring that is stretched 1 in. by a force of 100 lb. A force F0cosωtF0cosωt acts on the mass. At what frequency (in hertz) will resonance oscillations occur? Neglect damping.
A front-loading washing machine is mounted on a thick rubber pad that acts like a spring; the weight W=mgW=mg (with g=9.8m/s2g=9.8m/s2) of the machine depresses the pad exactly 0.50.5 cm. When its rotor spins at ωω radians per second, the rotor exerts a vertical force F0cosωtF0cosωt newtons on the machine. At what speed (in revolutions per minute) will resonance vibrations occur? Neglect friction.
Pendulum-spring systemFigure5.6.10 shows a mass m on the end of a pendulum (of length L) also attached to a horizontal spring (with constant k). Assume small oscillations of m so that the spring remains essentially horizontal and neglect damping. Find the natural circular frequency ω0ω0 of motion of the mass in terms of L, k, m, and the gravitational constant g.
Pulley-spring system A mass m hangs on the end of a cord around a pulley of radius a and moment of inertia I, as shown in Fig.5.6.11. The rim of the pulley is attached to a spring (with constant k). Assume small oscillations so that the spring remains essentially horizontal and neglect friction. Find the natural circular frequency of the system in terms of m, a, k, I, and g.
Earthquake A building consists of two floors. The first floor is attached rigidly to the ground, and the second floor is of mass m=1000m=1000 slugs (fps units) and weighs 16 tons (32,000 lb). The elastic frame of the building behaves as a spring that resists horizontal displacements of the second floor; it requires a horizontal force of 5 tons to displace the second floor a distance of 1 ft. Assume that in an earthquake the ground oscillates horizontally with amplitude A0A0 and circular frequency ω,ω, resulting in an external horizontal force F(t)=mA0ω2sinωtF(t)=mA0ω2sinωt on the second floor. (a) What is the natural frequency (in hertz) of oscillations of the second floor? (b) If the ground undergoes one oscillation every 2.25 s with an amplitude of 3 in., what is the amplitude of the resulting forced oscillations of the second floor?
A mass on a spring without damping is acted on by the external force F(t)=F0cos3ωt.F(t)=F0cos3ωt. Show that there are two values of ωω for which resonance occurs, and find both.
Derive the steady periodic solution of
mx″+cx′+kx=F0sinωt.
mx''+cx'+kx=F0sinωt.
In particular, show that it is what one would expect—the same as the formula in (20) with the same values of C and ω,ω, except with sin(ωt−α)sin(ωt−α) in place of cos(ωt−α)cos(ωt−α).
Given the differential equation
mx″+cx′+kx=E0cosωt+F0sinωt.
mx''+cx'+kx=E0cosωt+F0sinωt.
—with both cosine and sine forcing terms—derive the steady periodic solution
where αα is defined in Eq.(22) and β=tan−1(F0/E0).β=tan−1(F0/E0). (Suggestion: Add the steady periodic solutions separately corresponding to E0cosωtE0cosωt and F0sinωtF0sinωt (see Problem25).)
According to Eq.(21), the amplitude of forced steady periodic oscillations for the system mx″+cx′+kx=F0cosωtmx''+cx'+kx=F0cosωt is given by
C(ω)=F0√(k−mω2)2+(cω)2.
C(ω)=F0(k−mω2)2+(cω)2−−−−−−−−−−−−−−−√.
(a) If c≧ccr/√2,c≧ccr/2–√, where ccr=√4km,ccr=4km−−−−√, show that C steadily decreases as ωω increases. (b) If c<ccr/√2,c<ccr/2–√, show that C attains a maximum value (practical resonance) when
ω=ωm=√km−c22m2<ω0=√km.
ω=ωm=km−c22m2−−−−−−−−−√<ω0=km−−−√.
As indicated by the cart-with-flywheel example discussed in this section, an unbalanced rotating machine part typically results in a force having amplitude proportional to the square of the frequency ω.ω.(a) Show that the amplitude of the steady periodic solution of the differential equation
mx″+cx′+kx=mAω2cosωt
mx''+cx'+kx=mAω2cosωt
(with a forcing term similar to that in Eq.(17)) is given by
C(ω)=mAω2√(k−mω2)2+(cω)2.
C(ω)=mAω2(k−mω2)2+(cω)2−−−−−−−−−−−−−−−√.
(b) Suppose that c2<2mk.c2<2mk. Show that the maximum amplitude occurs at the frequency ωmωm given by
ωm=√km(2mk2mk−c2).
ωm=km(2mk2mk−c2)−−−−−−−−−−−−−√.
Thus the resonance frequency in this case is larger (in contrast with the result of Problem27) than the natural frequency ω0=√k/m.ω0=k/m−−−−√. (Suggestion: Maximize the square of C.)
Automobile Vibrations
Problems 29 and 30 deal further with the car of Example5. Its upward displacement function satisfies the equationmx″+cx′+kx=cy′+kymx''+cx'+kx=cy'+kywhen the shock absorber is connected (so thatc>0c>0). Withy=asinωty=asinωtfor the road surface, this differential equation becomes
mx″+cx′+kx=E0cosωt+F0sinωt
mx''+cx'+kx=E0cosωt+F0sinωt
whereE0=cωaE0=cωaandF0=kaF0=ka.
Apply the result of Problem26 to show that the amplitude C of the resulting steady periodic oscillation for the car is given by
Because ω=2πv/Lω=2πv/L when the car is moving with velocity v, this gives C as a function of v.
Figure5.6.12 shows the graph of the amplitude function C(ω)C(ω) using the numerical data given in Example5 (including c=3000 N·s/mc=3000 N⋅s/m). It indicates that, as the car accelerates gradually from rest, it initially oscillates with amplitude slightly over 5 cm. Maximum resonance vibrations with amplitude about 14 cm occur around 32 mi/h, but then subside to more tolerable levels at high speeds. Verify these graphically based conclusions by analyzing the function C(ω).C(ω). In particular, find the practical resonance frequency and the corresponding amplitude.
FIGURE5.6.12.
Amplitude of vibrations of the car on a washboard surface.
5.6 Application Forced Vibrations
Here we investigate forced vibrations of the mass–spring–dashpot system with equation
mx″+cx′+kx=F(t).
mx''+cx'+kx=F(t).
(1)
To simplify the notation, let’s take m=p2,c=2p,m=p2,c=2p, and k=p2q2+1,k=p2q2+1, where p>0p>0 and q>0.q>0. Then the complementary function of Eq.(1) is
xc(t)=e−t/p(c1cosqt+c2sinqt).
xc(t)=e−t/p(c1cosqt+c2sinqt).
(2)
We will take p=5,q=3,p=5,q=3, and thus investigate the transient and steady periodic solutions corresponding to
25x″+10x′+226x=F(t),x(0)=0,x′(0)=0
25x''+10x'+226x=F(t),x(0)=0,x'(0)=0
(3)
with several illustrative possibilities for the external force F(t). For your personal investigations to carry out similarly, you might select integers p and q with 6≦p≦96≦p≦9 and 2≦q≦52≦q≦5.
Investigation 1: With periodic external force F(t)=901cos3t,F(t)=901cos3t, the Matlab commands
x = dsolve(′25*D2x+10*Dx+226*x=901*cos(3*t)′,
′x(0)=0, Dx(0)=0′);
x = simple(x);
syms t, xsp = cos(3*t) + 30*sin(3*t);
ezplot(x, [0 6*pi]),hold on
ezplot(xsp, [0 6*pi])
produce the plot shown in Fig.5.6.13. We see the (transient plus steady periodic) solution
x(t)=cos3t+30sin3t+e−t/5(−cos3t−45115sin3t)
x(t)=cos3t+30sin3t+e−t/5(−cos3t−45115sin3t)
rapidly “building up” to the steady periodic oscillation xsp(t)=cos3t+30sin3t.xsp(t)=cos3t+30sin3t..
FIGURE5.6.13.
The solution x(t)=xtr(t)+xsp(t)x(t)=xtr(t)+xsp(t) and the steady periodic solution x(t)=xsp(t)x(t)=xsp(t) with periodic external force F(t)=901cos3tF(t)=901cos3t.
Investigation 2: With damped oscillatory external force
F(t)=900e−t/5cos3t,
F(t)=900e−t/5cos3t,
we have duplication with the complementary function in (2). The Maple commands
de2 := 25*diff(x(t),t,t)+10*diff(x(t),t)+226*x(t) =
900*exp(-t/5)*cos(3*t);
dsolve({de2,x(0)=0,D(x)(0)=0}, x(t));
x := simplify(combine(rhs(%),trig));
C := 6*t*exp(-t/5);
plot({x,C,-C},t=0..8*Pi);
produce the plot shown in Fig.5.6.14. We see the solution
x(t)=6te−t/5sin3t
x(t)=6te−t/5sin3t
oscillating up and down between the envelope curves x=±6te−t/5.x=±6te−t/5. (Note the factor of t that signals a resonance situation.)
FIGURE5.6.14.
The solution x(t)=6te−t/5x(t)=6te−t/5 and the envelope curves x(t)=±6te−t/5x(t)=±6te−t/5 with damped oscillatory force F(t)=900−t/5cos3tF(t)=900−t/5cos3t.
Investigation 3: With damped oscillatory external force
F(t)=2700te−t/5cos3t,
F(t)=2700te−t/5cos3t,
we have a still more complicated resonance situation. The Mathematica commands
produce the plot shown in Fig.5.6.15. We see the solution
x(t)=e−t/5[3tcos3t+(9t2−1)sin3t]
x(t)=e−t/5[3tcos3t+(9t2−1)sin3t]
oscillating up and down between the envelope curves
x=±e−t/5√(3t)2+(9t2−1)2.
x=±e−t/5(3t)2+(9t2−1)2−−−−−−−−−−−−−−√.
FIGURE5.6.15.
The solution x(t)=e−t/5[3tcos3t+(9t2−1)sin3t]x(t)=e−t/5[3tcos3t+(9t2−1)sin3t] and the envelope curves x=±e−t/5√(3t)2+(9t2−1)2x=±e−t/5(3t)2+(9t2−1)2−−−−−−−−−−−−−−√ with external force F(t)=2700te−t/5cos3tF(t)=2700te−t/5cos3t.